# STC SA2471NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Safran Cabin Inc., United States - Description: Installation of centerline bin, overhead side bin. - Applied: September 25, 1984 - Status date: July 18, 2025 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) - Certificate PDF: https://openairdocs.org/files/sha256/06/16/06166b87fd9c5dd3ceb54011257aac0f9d8d7c335574d3f9c7219ef5f4734522 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189917225920260112191803.0001 - DRS record last changed: January 12, 2026 - Page: https://openairdocs.org/stc/SA2471NM ## ADs that name it (0) None. ## Approved models (3) - The Boeing Company DC-10-10 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) - The Boeing Company DC-10-30 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) - The Boeing Company DC-10-40 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2471NM This certificate issued to: Safran Cabin Inc. 7330 Lincoln Way Garden Grove, CA 92841 Part 25 of Title 14, Code of Federal Regulations Type Certificate Number: A22WE Original Product Make: McDonnell Douglas Corporation Description of Type Design Change: Model: DC-10-10, -30, -40 Installation of Centerline Bin and/or Overhead Side Bin in accordance with FAA sealed Index List No. 1196, Revision N/C, dated December 21, 1988, or later FAA sealed revision; or Installation of Centerline Bin and/or Overhead Side Bin and/or Overhead Side Bin and/or Curtain, in accordance with FAA approved Index List No. 1196, Revision E, dated May 16, 1991, or Installation of Centerline Bin and/or Curtain and/or Outboard Bin, in accordance with FAA approved Index List No. 1196, Revision F, dated October 12, 1998, or later FAA approved revision. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above note airplane model series only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of Application: 09/25/1984 Date Reissued: 11/12/1993 12/29/2005 12/03/2018 Date of Issuance: 02/13/1985 Date Amended: 04/25/1985 02/07/1989 11/25/1998 A see continuation sheet for additional dates By Direction of the Administrator Signature: Title: ODA Administrator, ODA-606394-NM United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2471NM Effective Date: 07/18/2025 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2471NM Effective Date: 07/18/2025 Date Reissued: - cont.: 07/18/2025 ---END--- ## Every issue (2) - July 18, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/06/16/06166b87fd9c5dd3ceb54011257aac0f9d8d7c335574d3f9c7219ef5f4734522) - December 29, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dc/1d/dc1d829c885b3b3b1bdbd23c2d020e50f8794f5d0f1aebb2bd2bb553ba921118) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.